首页|融合空域下基于ADS-B IN的无人机防撞研究

融合空域下基于ADS-B IN的无人机防撞研究

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基于无人机未来融入国家空域系统的发展趋势,针对无人机数量增多导致与有人机之间碰撞风险增大的问题,根据ADS-B IN的优势和特点,提出了一种融合空域下,无人机利用ADS-BIN进行冲突探测和解脱的模型.模型中依据飞行器的具体参数划设了有人机的安全区和保护区,并利用几何法设置潜在碰撞风险判定标准和解脱完成标准,根据最小机动和最快解脱原则,无人机在空域内进行实时探测并对可能产生冲突的有人机主动避让,在避让过程中分别考虑了速度解脱、航向解脱、速度和航向混合解脱三种解脱策略.在实际运行场景中,同时考虑了风对航空器速度和航向的影响,进行了风速修正.设置三种运行场景进行了仿真试验,仿真结果满足最低安全间隔的要求.为进一步验证模型的优势,另与传统的人工势场方法进行了仿真对比.以上两种结果均证实了模型的可靠性和优越性,未来可用于降低管制员工作负荷,提高空域整体安全性.
ADS-B IN-based UAV collision avoidance study in converged airspace
Based on the future development trend of Unmanned Aerial Vehicles(UAVs)integrating into the national airspace system,and in response to the increasing collision risk between UAVs and manned aircraft due to the growing number of UAVs,following the advantages and characteristics of high update rate and low energy consumption of ADS-B IN,it is considered to install it on UAVs with high maneuverability.This proposal aims to use ADS-B IN for collision detection and resolution in the fused airspace.In this model,safety and protection zones for manned aircraft are defined based on specific aircraft parameters.Criteria for determining the potential collision risk and the completion conditions for collision resolution are established based on the magnitude and direction of the relative velocity between the two aircraft.Following the principles of minimal maneuvering and the quickest resolution,the UAV carries out real-time detection in the airspace and actively avoids potential conflicts with manned aircraft.During the avoidance process,three kinds of relief strategies,namely speed relief,heading relief,and a combination of speed and heading relief,are respectively considered.All three relief strategies are designed to make the relative speeds coincide with the boundaries of collision cones.In practical scenarios,the model takes into account the influence of wind on aircraft speed and heading at the same time,and the wind speed correction is carried out.In the article,three operation scenarios are set up for simulation experiments,and the final results of the simulation satisfy the requirement of minimum safety interval.Additionally,to further verify the superiority and reliability of the model and ensure the model's advancement,another choice is conducted to compare the simulation with the traditional artificial potential field method.Both results confirm the reliability and superiority of the model,which can be used in the future to release fusion operation and reduce the workload of controllers as well as enhance the overall safety of the airspace.

safety engineeringconflict resolutiongeometric methodsUnmanned Aerial Vehicle(UAV)aviation safety

王莉莉、闵幸兴

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中国民航大学空中交通管理学院,天津 300300

安全工程 冲突解脱 几何法 无人机 航空安全

国家重点研发计划项目国家自然科学基金委员会与中国民用航空局联合资助项目

2022YFB4300904U1633124

2024

安全与环境学报
北京理工大学 中国环境科学学会 中国职业安全健康协会

安全与环境学报

CSTPCD北大核心
影响因子:0.943
ISSN:1009-6094
年,卷(期):2024.24(7)